유한요소법에 의한 복합적층 원통쉘의 좌굴해석Buckling Analysis of Laminated Composite Cylindrical Shell by the Finite Element Method
- Publisher
- 한국항공우주학회
- Issue Date
- 1984-04
- Language
- Korean
- Citation
한국항공우주학회지, v.12, no.1, pp.85 - 94
- ISSN
- 1225-1348
- Appears in Collection
- AE-Journal Papers(저널논문)
- Files in This Item
- There are no files associated with this item.
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